Analysis and conceptual design of micro class UAV for aerodesign international competition

• Autorzy: Figur K. , Lorenc W. , Nykaza A.

Identyfikatory

DOI

10.5604/01.3001.0010.2805

• Języki publikacji: EN

Abstrakty

EN

Aero Design is an annual student competition held by Society of Automotive Engineers in which the goal is to design and build a flying UAV capable of lifting the highest payload while observing lowest payload weight and fitting in a specified carrying case. To achieve that task teams have to choose between conflicting objectives that are lowest empty weight and highest lifting capacity. The rules state that design to enter the competition must be a fixed wing aircraft fitting in a box with inside dimensions of 24x18x8 inches. The payload bay has to be a rectangular block measuring 5x2x2 inches. There also is a limit of 55 pounds total weight with payload. The aircraft must take of either by hand launch or be propelled using a rubber tubing, than do a 360-degree circuit of the flying field and finally land within 200 feet landing zone. The article presents requirements analysis, weather research, design research, considered about launch method, wing layout and aircraft layout study (napkin sketches).

Słowa kluczowe

EN

UAV; unmanned aerial vehicle; drone; analysis; aircraft design

PL

bezzałogowy statek powietrzny; dron; analiza; projekt samolotu

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2017
• Tom: Vol. 24, No. 1
• Strony: 129--135
• Opis fizyczny: Bibliogr. 5 poz., rys.

Twórcy

autor

Figur K.

• Air Force Institute of Technology Department of Aircraft and Helicopters Ksiecia Boleslawa 6, 01-494 Warszawa, Poland tel.:[phone], fax: [phone]

autor

Lorenc W.

• Air Force Institute of Technology Department of Aircraft and Helicopters Ksiecia Boleslawa 6, 01-494 Warszawa, Poland tel.:[phone], fax: [phone]

autor

Nykaza A.

• Poznan University of Technology Mari Skłodowskiej-Curie 5, 60-965 Poznan, Poland tel.: [phone], fax: [phone]

Bibliografia

• [1] Vas, E., Lescroel, A., Duriez, O., Boguszewski, G., Gremillet, D., Approaching birds with drones: first experiments and ethical guidelines, Biology Letters, Vol. 11, Is. 2, 2015.
• [2] Fueyo, Engineering Turbulence Modelling and Experiments 5, Malorca, Spain 2002.
• [3] Spalart, P. R., Allmaras, S. R., A One-Equation Turbulence Model for Aerodynamic Flows,AIAA Paper 92-0439, 1992.
• [4] Wilcox, D. C., Turbulence Modeling for CFD, DCW Industries, Inc., La Canada, CA.
• [5] Flaga, A., Błazik-Borowa, E., Podgórski, J., Aerodynamika smukłych budowli I konstrukcji prętowo-cięgnowych, Wydawnictwo Politechniki Lubelskiej, Lublin 2004.

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).